Please use this identifier to cite or link to this item: http://dspace.mediu.edu.my:8181/xmlui/handle/1721.1/3694
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dc.creatorTan, Bui-Thanh-
dc.creatorWillcox, Karen E.-
dc.creatorDamodaran, Murali-
dc.date2003-11-17T17:08:20Z-
dc.date2003-11-17T17:08:20Z-
dc.date2003-01-
dc.date.accessioned2013-10-09T02:32:03Z-
dc.date.available2013-10-09T02:32:03Z-
dc.date.issued2013-10-09-
dc.identifierhttp://hdl.handle.net/1721.1/3694-
dc.identifier.urihttp://koha.mediu.edu.my:8181/xmlui/handle/1721-
dc.descriptionTwo extensions to the proper orthogonal decomposition (POD) technique are considered for steady transonic aerodynamic applications. The first is to couple the POD approach with a cubic spline interpolation procedure in order to develop fast, low-order models that accurately capture the variation in parameters, such as the angle of attack or inflow Mach number. The second extension is a POD technique for the reconstruction of incomplete or inaccurate aerodynamic data. First, missing flow field data is constructed with an existing POD basis constructed from complete aerodynamic data. Second, a technique is used to develop a complete snapshots from an incomplete set of aerodynamic snapshots.-
dc.descriptionSingapore-MIT Alliance (SMA)-
dc.format1620170 bytes-
dc.formatapplication/pdf-
dc.languageen_US-
dc.relationHigh Performance Computation for Engineered Systems (HPCES);-
dc.subjectProper Orthogonal Decomposition-
dc.subjectinviscid transonic aerodynamics-
dc.subjectflow fields-
dc.subjectcubic spline interpolation procedure-
dc.titleApplications of Proper Orthogonal Decomposition for Inviscid Transonic Aerodynamics-
dc.typeArticle-
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